CN112629329A - Fighting robot - Google Patents

Fighting robot Download PDF

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Publication number
CN112629329A
CN112629329A CN202011413206.9A CN202011413206A CN112629329A CN 112629329 A CN112629329 A CN 112629329A CN 202011413206 A CN202011413206 A CN 202011413206A CN 112629329 A CN112629329 A CN 112629329A
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CN
China
Prior art keywords
machine body
air
air bag
blocking
motor
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Withdrawn
Application number
CN202011413206.9A
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Chinese (zh)
Inventor
康望才
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Hunan Hankun Industrial Co Ltd
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Hunan Hankun Industrial Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
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Application filed by Hunan Hankun Industrial Co Ltd filed Critical Hunan Hankun Industrial Co Ltd
Priority to CN202011413206.9A priority Critical patent/CN112629329A/en
Publication of CN112629329A publication Critical patent/CN112629329A/en
Withdrawn legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00Means of attack or defence not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25JMANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J11/00Manipulators not otherwise provided for
    • B25J11/002Manipulators for defensive or military tasks

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Engineering & Computer Science (AREA)
  • Robotics (AREA)
  • Mechanical Engineering (AREA)
  • Manipulator (AREA)

Abstract

The invention discloses a combat robot, which comprises a body mechanism, a posture adjusting mechanism, an adsorption mechanism, a drilling mechanism, a blocking mechanism and a power driving mechanism, wherein the body mechanism comprises a front body and a rear body; the drilling mechanism is arranged in the adsorption mechanism; the adsorption mechanism is connected with one ends of the front air bags, the other ends of the front air bags are connected with one end of the front machine body, the other end of the front machine body is connected with one ends of the rear air bags, the other ends of the rear air bags are connected with one end of the rear machine body, and the other end of the rear machine body is connected with the blocking air bags; the front air bag, the rear air bag and the blocking air bag are the same in number and opposite in position. The invention has simple structure, low manufacturing cost and flexible and convenient use.

Description

Fighting robot
Technical Field
The invention relates to the technical field of weaponry, in particular to a combat robot.
Background
The traditional weapon equipment is expensive, the technological innovation cost is extremely high, and firstly, a large number of technological talents are needed to be buried and dried, and expensive test equipment is matched. The second is a long weapon development cycle, which is enough to push the price of the weapon equipment up to the point of letting the people to smoke the tongue. Therefore, the existing weaponry is expensive, which is a technical problem to be solved urgently.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides the fighting robot which is simple in structure, low in manufacturing cost and flexible and convenient to use.
In order to achieve the purpose, the invention provides a combat robot, which comprises a body mechanism, a posture adjusting mechanism, an adsorption mechanism, a drilling mechanism, a blocking mechanism and a power driving mechanism, wherein the body mechanism comprises a front body and a rear body, the posture adjusting mechanism comprises a front air bag, a rear air bag, a front air pump and a rear air pump, and the blocking mechanism comprises a blocking air bag;
the drilling mechanism is arranged in the adsorption mechanism; the adsorption mechanism is connected with one ends of the front air bags, the other ends of the front air bags are connected with one end of the front machine body, the other end of the front machine body is connected with one ends of the rear air bags, the other ends of the rear air bags are connected with one end of the rear machine body, and the other end of the rear machine body is connected with the blocking air bags; the front air bag, the rear air bag and the blocking air bag are the same in number and opposite in position in sequence;
the power driving mechanisms are arranged in the front machine body and the rear machine body; the number of the front air pumps is multiple and is the same as that of the front air bags and the rear air bags, the front air pumps are arranged on the front machine body, and two first air vents of the front air pumps are respectively connected with the front air bags and the rear air bags;
the number of the rear air pumps is multiple and is the same as that of the rear air bags and the blocking air bags, the rear air pumps are arranged on the rear machine body, and two second air ports of the rear air pumps are respectively connected with the rear air bags and the blocking air bags;
in an initial state, the front air bag, the rear air bag and the blocking air bag are filled with air, the blocking air bag is provided with a folded part, and the folded part is in a folded and contracted state; when the blocking air bag is in a blocking state, air in the front air bag and the rear air bag is inflated into the blocking air bag, so that the fold part is expanded outwards.
Furthermore, the power driving mechanism comprises a driving motor, a mounting seat, a propeller and a power driving mechanism positioned in the front machine body, wherein the mounting seat is connected with the front machine body, the power driving mechanism is positioned in the rear machine body, and the mounting seat is connected with the rear machine body; the driving motor is installed on the installation seat, the propeller is connected with the driving motor, and the liquid in the machine body mechanism flows from the front machine body to the rear machine body.
Furthermore, the number of the driving motors and the number of the propellers in the front machine body and the rear machine body are two, and the driving motors are arranged on two sides of the mounting seat.
Furthermore, the adsorption mechanism comprises a flexible sucker, a valve plate, a connecting rod, a valve seat, an electromagnet and a mounting rack, one end of the valve seat is connected with one end of the front airbags, and the other end of the valve seat is connected with the flexible sucker; the other end of the valve seat is provided with the mounting frame, the electromagnet is mounted on the mounting frame, and the electromagnet is positioned in the flexible sucker;
the valve seat is provided with a water inlet communicated with the interior of the machine body mechanism, the valve plate is movably arranged in the valve seat and used for closing/opening the water inlet, the valve plate is connected with the connecting rod, and the connecting rod is arranged in the flexible sucker; the flexible sucker can stretch out and draw back, and the connecting rod and the valve plate move relative to the valve seat along with the stretching of the flexible sucker so as to open/close the water inlet hole.
Further, the drilling mechanism comprises a motor, a drill bit, a spring and a clamping jaw, the motor is mounted on the mounting frame, an output shaft of the motor is movably matched and connected with a handle part of the drill bit, the handle part of the drill bit is of a hollow structure, and the spring is arranged in the handle part of the drill bit; two ends of the spring are respectively connected with an output shaft of the motor and the drill bit; the outer surface of the handle part of the drill bit is provided with a jaw groove, and one end of the jaw is elastically and rotatably connected with one end, close to the drill bit, of the jaw groove; the jaws are flared relative to the shank of the drill bit.
Further, the motor is a double-head output motor, an output shaft of the double-head output motor is movably matched and connected with the handle part of the drill bit, and another output shaft of the double-head output motor is connected with the propeller.
Furthermore, explosive bags are arranged on the front machine body and the rear machine body.
The combat robot is submerged in water, the combat robot is driven to move in the water through the power driving mechanism, and in an initial state, the front air bag, the rear air bag and the blocking air bag are filled with air, wherein the folded part is in a folded and contracted state. The air in the front air bag is inflated into the rear air bag through the front air pump, so that the air amount in the rear air bags is different, and the rear air bags are bent; air in will back gasbag is changeed through back air pump and is inflated to blocking the gasbag in to make a plurality of air volumes that block in the gasbag different, a plurality of gasbag that block take place the bending, so in order to realize the change of operation robot gesture, make operation robot can follow not equidirectional motion, the flexibility ratio is high.
When the combat robot is close to the enemy ship body, the combat robot is effectively adsorbed on the enemy ship body through the adsorption mechanism, and after adsorption, the enemy ship body is drilled and damaged through the drilling mechanism. In drilling mechanism and adsorption mechanism working process simultaneously, preceding air pump and back air pump action to all change the air in preceding gasbag, the back gasbag and fill to stopping in the gasbag, make fold portion outwards strutted, hinder the area greatly increased of mechanism, when the enemy hull was moved this moment, hinder the mechanism and can give great resistance, lead to enemy hull operation difficulty, so when a plurality of fighter robot was attacked to the enemy hull simultaneously, the enemy hull can't be moved very fast, enemy hull destruction degree greatly increased.
The invention has simple integral structure, effectively reduces the manufacturing cost, and simultaneously adopts the low-price combat robot to attack the expensive hull of the enemy, so that the enemy economy is greatly damaged.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a perspective view of the present invention, in which the wrinkle part is in a state of shrinking wrinkles.
Fig. 2 is a perspective view of the cut-out section of fig. 1, in which the fold portion is in an outwardly expanded state.
Fig. 3 is a perspective view of the suction mechanism and the drilling mechanism of fig. 1.
Fig. 4 is a partial perspective view of fig. 3.
Fig. 5 is a perspective view of fig. 3 cut away.
FIG. 6 is a perspective view of the interference mechanism of the present invention with the pleats in a collapsed state.
Detailed Description
The following detailed description of the present invention is given for the purpose of better understanding technical solutions of the present invention by those skilled in the art, and the present description is only exemplary and explanatory and should not be construed as limiting the scope of the present invention in any way.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
It is to be understood that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like are used in a generic and descriptive sense only and not for purposes of limitation, the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like are used in the generic and descriptive sense only and not for purposes of limitation, as the term is used in the generic and descriptive sense, and not for purposes of limitation, unless otherwise specified or implied, and the specific reference to a device or element is intended to be a reference to a particular element, structure, or component. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1 to 6, the present embodiment provides a fighter robot, which includes a fuselage mechanism 1, a posture adjusting mechanism, an adsorption mechanism 4, a drilling mechanism 5, a blocking mechanism, and a power driving mechanism 2, wherein the fuselage mechanism 1 includes a front fuselage 10 and a rear fuselage 11, the posture adjusting mechanism includes a front airbag 30, a rear airbag 31, a front air pump 33, and a rear air pump 34, and the blocking mechanism includes a blocking airbag 32;
the drilling mechanism 5 is arranged in the adsorption mechanism 4; the adsorption mechanism 4 is connected with one end of the plurality of front airbags 30, the other end of the plurality of front airbags 30 is connected with one end of the front body 10, the other end of the front body 10 is connected with one end of the plurality of rear airbags 31, the other end of the plurality of rear airbags 31 is connected with one end of the rear body 11, and the other end of the rear body 11 is connected with the plurality of barrier airbags 32; the front air bags 30, the rear air bags 31 and the blocking air bags 32 are the same in number and opposite in position in sequence;
the power driving mechanism 2 is arranged in the front machine body 10 and the rear machine body 11; the number of the front air pumps 33 is multiple and is the same as that of the front air bags 30 and the rear air bags 31, the multiple front air pumps 33 are installed on the front fuselage 10, and two first air vents of the front air pumps 33 are respectively connected with the front air bags 30 and the rear air bags 31;
the number of the rear air pumps 34 is multiple and is the same as that of the rear air bags 31 and the blocking air bags 32, the rear air pumps 34 are installed on the rear machine body 11, and two second air vents of the rear air pumps 34 are respectively connected with the rear air bags 31 and the blocking air bags 32;
in an initial state, the front airbag 30, the rear airbag 31 and the barrier airbag 32 are filled with air, a folded part 320 is arranged on the barrier airbag 32, and the folded part 320 is in a folded and contracted state (as shown in fig. 1); when the baffle air bag 32 is in the baffle state, the air in the front air bag 30 and the rear air bag 31 is inflated into the baffle air bag 32, so that the fold portion 320 is expanded outwards (as shown in fig. 2).
When the embodiment is used, the fighter robot is submerged in water, the fighter robot is driven to move in the water by the power driving mechanism 2, and in an initial state, the front air bag 30, the rear air bag 31 and the blocking air bag 32 are filled with air, wherein the folded part 320 is in a folded and contracted state. The air in the front airbag 30 is inflated into the rear airbag 31 by the front air pump 33, so that the air amount in the plurality of rear airbags 31 is different and the plurality of rear airbags 31 are bent, and correspondingly, the air in the rear airbag 31 is inflated into the front airbag 30 by the front air pump 33, so that the air amount in the plurality of front airbags 30 is different and the plurality of front airbags 30 are bent; air in will back gasbag 31 is changeed through back air pump 34 and is inflated to blocking in the gasbag 32 to make a plurality of air volumes that block in the gasbag 32 different, a plurality of gasbag 32 that block take place the bending, so in order to realize the change of fighter robot gesture, make fighter robot can follow not equidirectional motion, the flexibility ratio is high.
When the combat robot of the embodiment is close to the enemy ship body, the combat robot is effectively adsorbed on the enemy ship body through the adsorption mechanism 4, and after adsorption, the enemy ship body is drilled and destroyed through the drilling mechanism 5. Meanwhile, in the working process of the drilling mechanism 5 and the adsorption mechanism 4, the front air pump 33 and the rear air pump 34 act to completely transfer and inflate the air in the front air bag 30 and the rear air bag 31 into the blocking air bag 32, so that the folded part 320 is outwards expanded, the area of the blocking mechanism is greatly increased, and when the enemy ship body runs, the blocking mechanism can provide great resistance to the running of the enemy ship body, so that the enemy ship body is difficult to run.
Further preferably, in this embodiment, the power driving mechanism 2 includes a driving motor 21, a mounting base 20, a propeller 22, and the power driving mechanism 2 is located in the front body 10, the mounting base 20 is connected to the front body 10, the power driving mechanism 2 is located in the rear body 11, and the mounting base 20 is connected to the rear body 11; the driving motor 21 is installed on the installation base 20, the propeller 22 is connected with the driving motor 21, and the liquid in the machine body mechanism 1 flows from the front machine body 10 to the rear machine body 11. The propeller 22 is driven by the drive motor 21 to move, so that water flows in from the front inside the body mechanism 1 and is discharged from the rear.
In this embodiment, it is preferable that the number of the driving motors 21 and the propellers 22 in the front body 10 and the rear body 11 is two, and the two driving motors 21 are installed on both sides of the mounting base 20 to increase the driving force of the power driving mechanism 2.
Further preferably, the suction mechanism 4 includes a flexible suction cup 40, a valve plate 42, a connecting rod 43, a valve seat 41, an electromagnet 44, and a mounting bracket 45, wherein one end of the valve seat 41 is connected to one end of the front airbags 30, and the other end of the valve seat 41 is connected to the flexible suction cup 40; the other end of the valve seat 41 is provided with the mounting rack 45, the electromagnet 44 is mounted on the mounting rack 45, and the electromagnet 44 is positioned in the flexible sucker 40; the valve seat 41 is provided with a water inlet 410 hole communicated with the interior of the machine body mechanism 1, the valve plate 42 is movably arranged in the valve seat 41 and is used for closing/opening the water inlet 410, the valve plate 42 is connected with the connecting rod 43, and the connecting rod 43 is arranged in the flexible sucker 40; the flexible suction cup 40 can be extended and contracted, and the connecting rod 43 and the valve plate 42 move relative to the valve seat 41 as the flexible suction cup 40 is extended and contracted to open/close the water inlet hole 410. Wherein the valve seat 41 is provided with a moving groove 411 matched with the valve plate 42.
In the embodiment, when the combat robot does not contact with the enemy ship, the flexible suction cup 40 is in a natural state, the water inlet hole 410 is in an open state, the power driving mechanism 2 works, and water enters from the central hole 410 of the flexible suction cup 40, passes through the valve seat 41, the front air bag 30, the front body 10, the rear air bag 31, the rear body 11 and the blocking air bag 32 and then is discharged. When the power driving mechanism 2 is driven to the state that the adsorption mechanism 4 is in contact with the surface of the enemy ship, as the fighter robot continues to move towards the enemy ship, the flexible suction cups 40 are compressed, and as the flexible suction cups 40 are compressed, the connecting rods 43 and the valve plates 42 move relative to the valve seats 41 to close the water inlet holes 410, at this time, water can only flow in from the central holes of the flexible suction cups 40, so that the flexible suction cups 40 can be adsorbed on the enemy ship. Meanwhile, along with the compression of the flexible sucker 40, the electromagnet 44 can expose out of the surface of the flexible sucker 40, and the electromagnet 44 adsorbs the enemy ship body, so that the enemy ship body can be effectively adsorbed on the enemy ship body under the double adsorption action of the flexible sucker 40 and the electromagnet 44. In the present embodiment, the valve seat 41 is preferably provided with a plurality of water inlet holes 410, and a plurality of water inlet holes are provided corresponding to the number of the valve plates 42 and the connecting rods 43.
The embodiment further preferably includes that the drilling mechanism 5 includes a motor 50, a drill bit 51, a spring 53, and a latch 52, the motor 50 is mounted on the mounting frame 45, an output shaft of the motor 50 is movably connected with a handle of the drill bit 51 in a matching manner, the handle of the drill bit 51 is hollow, and the spring 53 is disposed in the handle of the drill bit 51; two ends of the spring 53 are respectively connected with the output shaft of the motor 50 and the drill bit 51; the outer surface of the handle of the drill bit 51 is provided with a jaw groove 510, and one end of the jaw 52 is elastically and rotatably connected with one end of the jaw groove 510 close to the drill bit 51; the jaws 52 are flared relative to the shank of the drill bit 51.
This embodiment is when adsorption apparatus 4 adsorbs on the enemy hull, and flexible suction cup 40 can be compressed, and along with the compression of flexible suction cup 40, drill bit 51 can expose flexible suction cup 40's surface, and motor 50 starts to drive drill bit 51 and rotates this moment to drill bit 51 is gone into to the enemy hull, and after drill bit 51 went into the enemy hull, jack catch 52 card was on the enemy hull, makes the fighter robot effectively fix on the enemy hull. In the embodiment, the output shaft of the motor 50 is elastically connected with the drill 51 through the spring 53 to play a role of floating drilling, so that the drill 51 is prevented from being broken when drilling due to rigid connection. In particular, the output shaft of the motor 50 is inserted into the handle of the drill 51, wherein the output shaft of the motor 50 and the handle of the drill 51 are provided with a limiting part, so that the output shaft of the motor 50 can only be limited in the handle of the drill 51.
In this embodiment, the motor 50 is preferably a double-head output motor, one output shaft of the double-head output motor is movably connected with the handle of the drill 51 in a matching manner, and the other output shaft of the double-head output motor is connected with the propeller 22.
In the present embodiment, preferably, the explosive packs 6 are mounted on the front body 10 and the rear body 11. When the fighter robot is fixed on the enemy ship body, the explosive bag 6 is started to blast the enemy ship body, so that the enemy ship body is completely destroyed.
This embodiment of course also includes a power supply for supplying power to the drive motor 21, the motor 50, the electromagnet 44, and the like, and a switch for controlling energization of the power supply; the ignition device for igniting the explosive package 6 is also included, which is conventional in the art, and is not essential to the present embodiment, and thus will not be described in detail.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are given by way of illustration of the principles of the present invention, and that various changes and modifications may be made without departing from the spirit and scope of the invention as defined by the appended claims. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1. A combat robot is characterized by comprising a body mechanism, a posture adjusting mechanism, an adsorption mechanism, a drilling mechanism, a blocking mechanism and a power driving mechanism, wherein the body mechanism comprises a front body and a rear body;
the drilling mechanism is arranged in the adsorption mechanism; the adsorption mechanism is connected with one ends of the front air bags, the other ends of the front air bags are connected with one end of the front machine body, the other end of the front machine body is connected with one ends of the rear air bags, the other ends of the rear air bags are connected with one end of the rear machine body, and the other end of the rear machine body is connected with the blocking air bags; the front air bag, the rear air bag and the blocking air bag are the same in number and opposite in position in sequence;
the power driving mechanisms are arranged in the front machine body and the rear machine body; the number of the front air pumps is multiple and is the same as that of the front air bags and the rear air bags, the front air pumps are arranged on the front machine body, and two first air vents of the front air pumps are respectively connected with the front air bags and the rear air bags;
the number of the rear air pumps is multiple and is the same as that of the rear air bags and the blocking air bags, the rear air pumps are arranged on the rear machine body, and two second air ports of the rear air pumps are respectively connected with the rear air bags and the blocking air bags;
in an initial state, the front air bag, the rear air bag and the blocking air bag are filled with air, the blocking air bag is provided with a folded part, and the folded part is in a folded and contracted state; when the blocking air bag is in a blocking state, air in the front air bag and the rear air bag is inflated into the blocking air bag, so that the fold part is expanded outwards.
2. The fighter robot of claim 1, wherein the power drive mechanism comprises a drive motor, a mounting base, a propeller, a power drive mechanism located in the front fuselage, the mounting base being connected to the front fuselage, a power drive mechanism located in the rear fuselage, the mounting base being connected to the rear fuselage; the driving motor is installed on the installation seat, the propeller is connected with the driving motor, and the liquid in the machine body mechanism flows from the front machine body to the rear machine body.
3. The fighter robot of claim 2, characterized in that the number of drive motors and propellers in the front fuselage and the rear fuselage is two, and the two drive motors are mounted on both sides of the mounting base.
4. The fighter robot of claim 2, wherein the suction mechanism comprises a flexible sucker, a valve plate, a connecting rod, a valve seat, an electromagnet and a mounting rack, one end of the valve seat is connected with one ends of the front airbags, and the other end of the valve seat is connected with the flexible sucker; the other end of the valve seat is provided with the mounting frame, the electromagnet is mounted on the mounting frame, and the electromagnet is positioned in the flexible sucker;
the valve seat is provided with a water inlet communicated with the interior of the machine body mechanism, the valve plate is movably arranged in the valve seat and used for closing/opening the water inlet, the valve plate is connected with the connecting rod, and the connecting rod is arranged in the flexible sucker; the flexible sucker can stretch out and draw back, and the connecting rod and the valve plate move relative to the valve seat along with the stretching of the flexible sucker so as to open/close the water inlet hole.
5. The fighter robot of claim 4, wherein the drilling mechanism comprises a motor, a drill bit, a spring and a jaw, the motor is mounted on the mounting frame, an output shaft of the motor is movably connected with a handle of the drill bit in a matching manner, the handle of the drill bit is of a hollow structure, and the spring is arranged in the handle of the drill bit; two ends of the spring are respectively connected with an output shaft of the motor and the drill bit; the outer surface of the handle part of the drill bit is provided with a jaw groove, and one end of the jaw is elastically and rotatably connected with one end, close to the drill bit, of the jaw groove; the jaws are flared relative to the shank of the drill bit.
6. The fighter robot of claim 5, characterized in that the motor is a double-ended output motor, one output shaft of the double-ended output motor is movably and cooperatively connected with the handle portion of the drill, and the other output shaft of the double-ended output motor is connected with the propeller.
CN202011413206.9A 2020-12-07 2020-12-07 Fighting robot Withdrawn CN112629329A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011413206.9A CN112629329A (en) 2020-12-07 2020-12-07 Fighting robot

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Application Number Priority Date Filing Date Title
CN202011413206.9A CN112629329A (en) 2020-12-07 2020-12-07 Fighting robot

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Publication Number Publication Date
CN112629329A true CN112629329A (en) 2021-04-09

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CN202011413206.9A Withdrawn CN112629329A (en) 2020-12-07 2020-12-07 Fighting robot

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Publication number Priority date Publication date Assignee Title
CN103112568A (en) * 2012-12-21 2013-05-22 浙江建林电子电气有限公司 Flexible aggressive mechanical octopus
CN105730541A (en) * 2016-03-17 2016-07-06 上海交通大学 Pneumatic multi-bag type soft wall-climbing robot and control method thereof
CN106938691A (en) * 2017-02-16 2017-07-11 浙江大学 Centrifugal impeller sucker under water
CN108608420A (en) * 2018-03-20 2018-10-02 南京理工大学 There is one kind ring to indulge myo-architectonic pneumatic soft robot
WO2019148943A1 (en) * 2018-02-02 2019-08-08 上海交通大学 Suspendable crawler-type underwater operations robot for extremely soft ground
CN110450928A (en) * 2019-08-15 2019-11-15 沈阳海人科技有限公司 A kind of underwater sucker of electric motor built-in
CN110510088A (en) * 2019-09-29 2019-11-29 中国科学院合肥物质科学研究院 A kind of Multifunctional biomimetic robotic fish
CN112032464A (en) * 2020-09-30 2020-12-04 浙江水利水电学院 Pneumatically-bent flexible pipeline robot and control method

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Publication number Priority date Publication date Assignee Title
CN103112568A (en) * 2012-12-21 2013-05-22 浙江建林电子电气有限公司 Flexible aggressive mechanical octopus
CN105730541A (en) * 2016-03-17 2016-07-06 上海交通大学 Pneumatic multi-bag type soft wall-climbing robot and control method thereof
CN106938691A (en) * 2017-02-16 2017-07-11 浙江大学 Centrifugal impeller sucker under water
WO2019148943A1 (en) * 2018-02-02 2019-08-08 上海交通大学 Suspendable crawler-type underwater operations robot for extremely soft ground
CN108608420A (en) * 2018-03-20 2018-10-02 南京理工大学 There is one kind ring to indulge myo-architectonic pneumatic soft robot
CN110450928A (en) * 2019-08-15 2019-11-15 沈阳海人科技有限公司 A kind of underwater sucker of electric motor built-in
CN110510088A (en) * 2019-09-29 2019-11-29 中国科学院合肥物质科学研究院 A kind of Multifunctional biomimetic robotic fish
CN112032464A (en) * 2020-09-30 2020-12-04 浙江水利水电学院 Pneumatically-bent flexible pipeline robot and control method

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Application publication date: 20210409